TY  - RPRT
TI  - Longitudinal Stability and Control Characteristics as Determined by the Rocket-Model Technique for an Inline, Cruciform, Canard Missile Configuration with a Low-Aspect-Ratio Wing Having Trailing-Edge Flap Controls for a Mach Number Range of 0.7 to 1.8
AU  - Baber, H. T., Jr.
AU  - Moul, M. T.
PY  - 1955
UR  - https://ntrs.nasa.gov/citations/19690067250
ID  - 19690067250
ER  -